Mathematical Modelling and Identification of a Quadrotor

Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent autonomous flight, a quadrotor dynamical model is presented in this work. The purpose of this study is to get a better understanding of its flight dynamics. It is an underactuated system. So, a simpl...

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Detalles Bibliográficos
Autores: Cárdenas R., César A., COLLAZOS MORALES, CARLOS ANDRES, P. Ospina, Juan, Sánchez, Joaquín F., Caro-Ruiz, Claudia, Hugo Grisales, Victor, Ariza Colpas, Paola Patricia, De-La-Hoz-Franco, Emiro, R. González, Ramón E.
Tipo de recurso: artículo
Estado:Versión aceptada para publicación
Fecha de publicación:2020
País:Colombia
Institución:Corporación Universidad de la Costa
Repositorio:Repositorio REDICUC
Idioma:inglés
OAI Identifier:oai:repositorio.cuc.edu.co:11323/7355
Acceso en línea:https://hdl.handle.net/11323/7355
https://doi.org/10.1007/978-3-030-58799-4_19
https://repositorio.cuc.edu.co/
Access Level:acceso abierto
Palabra clave:Quadrotor
VTOL
Flight dynamics
UAV
Descripción
Sumario:Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent autonomous flight, a quadrotor dynamical model is presented in this work. The purpose of this study is to get a better understanding of its flight dynamics. It is an underactuated system. So, a simplified and clear model is needed to implement controllers on these kind of unmanned aerial systems. In addition, a computational tool is used for validation purposes. For future works embedded or intelligent control systems can be developed to control them. Gyroscopic and some aerodynamics effects are neglected.